Not a pilot, but I thought stall recovery is done through nose down first. Turbine engines take some time to respond to throttle up command and thrust on a loaded commercial plane is limited anyhow.
An airframe is supposed to have a nose down tendencies upon stalling, which would make it recoverable.
The Max may be more prone to stalling, but no one in their right mind would design a commercial airliner which can’t be recovered from stall.
An airframe is supposed to have a nose down tendencies upon stalling, which would make it recoverable.
The Max may be more prone to stalling, but no one in their right mind would design a commercial airliner which can’t be recovered from stall.